RU2007105046A - MAIN AIRCRAFT CHASSIS BRACKET - Google Patents

MAIN AIRCRAFT CHASSIS BRACKET Download PDF

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Publication number
RU2007105046A
RU2007105046A RU2007105046/11A RU2007105046A RU2007105046A RU 2007105046 A RU2007105046 A RU 2007105046A RU 2007105046/11 A RU2007105046/11 A RU 2007105046/11A RU 2007105046 A RU2007105046 A RU 2007105046A RU 2007105046 A RU2007105046 A RU 2007105046A
Authority
RU
Russia
Prior art keywords
pivotally connected
suspension
lever
landing gear
holding
Prior art date
Application number
RU2007105046/11A
Other languages
Russian (ru)
Other versions
RU2371353C2 (en
Inventor
Олег Тимофеевич Чугунов (RU)
Олег Тимофеевич Чугунов
Original Assignee
Открытое акционерное общество "Нижегородский авиастроительный завод "Сокол" (RU)
Открытое акционерное общество "Нижегородский авиастроительный завод "Сокол"
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Открытое акционерное общество "Нижегородский авиастроительный завод "Сокол" (RU), Открытое акционерное общество "Нижегородский авиастроительный завод "Сокол" filed Critical Открытое акционерное общество "Нижегородский авиастроительный завод "Сокол" (RU)
Priority to RU2007105046/11A priority Critical patent/RU2371353C2/en
Publication of RU2007105046A publication Critical patent/RU2007105046A/en
Application granted granted Critical
Publication of RU2371353C2 publication Critical patent/RU2371353C2/en

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Landscapes

  • Axle Suspensions And Sidecars For Cycles (AREA)
  • Fluid-Damping Devices (AREA)

Claims (1)

Основная опора шасси летательного аппарата с полурычажной подвеской колес, содержащая телескопическую амортизационную стойку, шарнирно через ось вращения присоединенную к планеру, двухплечий рычаг с осью крепления колес(а), шарнирно соединенный со штоком амортизационной стойки, жесткое устройство (подкос), удерживающее переднее плечо двухплечего рычага, двухзвенник, шарнирно соединенный с корпусом телескопической амортизационной стойки и двухплечим рычагом, удерживающий шток стойки от поворота относительно ее корпуса, и силовое устройство уборки-выпуска опоры шасси (гидроцилиндр, ломающийся подкос, электромеханический привод и т.п.), отличающаяся тем, что верхний конец жесткого устройства, удерживающего переднее плечо двухплечего рычага, шарнирно соединен с планером в точке, не лежащей на оси вращения амортизационной стойки при уборке-выпуске опоры шасси.The main landing gear support of the aircraft with a half-suspension wheel suspension, containing a telescopic shock absorber, pivotally connected to the airframe through the axis of rotation, a two-arm lever with a wheel mounting axis (a), pivotally connected to the suspension strut rod, a rigid device (brace) holding the two-shoulder front shoulder a lever, a two-link, pivotally connected to the housing of the telescopic suspension strut and a two-arm lever, holding the rod stock from rotation relative to its body, and the power the cleaning and exhausting property of the landing gear support (hydraulic cylinder, breaking brace, electromechanical drive, etc.), characterized in that the upper end of the rigid device holding the front shoulder of the two shoulders of the lever is pivotally connected to the glider at a point that does not lie on the axis of rotation of the suspension strut when cleaning the landing gear support.
RU2007105046/11A 2007-02-09 2007-02-09 Main leg of aircraft undercarriage RU2371353C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2007105046/11A RU2371353C2 (en) 2007-02-09 2007-02-09 Main leg of aircraft undercarriage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2007105046/11A RU2371353C2 (en) 2007-02-09 2007-02-09 Main leg of aircraft undercarriage

Publications (2)

Publication Number Publication Date
RU2007105046A true RU2007105046A (en) 2008-08-20
RU2371353C2 RU2371353C2 (en) 2009-10-27

Family

ID=39747542

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2007105046/11A RU2371353C2 (en) 2007-02-09 2007-02-09 Main leg of aircraft undercarriage

Country Status (1)

Country Link
RU (1) RU2371353C2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2488523C2 (en) * 2008-12-05 2013-07-27 Мессье-Бюгатти-Довти Device to decrease aircraft undercarriage length

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2488523C2 (en) * 2008-12-05 2013-07-27 Мессье-Бюгатти-Довти Device to decrease aircraft undercarriage length

Also Published As

Publication number Publication date
RU2371353C2 (en) 2009-10-27

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Legal Events

Date Code Title Description
FZ9A Application not withdrawn (correction of the notice of withdrawal)

Effective date: 20081118

PC43 Official registration of the transfer of the exclusive right without contract for inventions

Effective date: 20180206

HE4A Change of address of a patent owner

Effective date: 20210121